forcesAndMoments
Class: Aero.FixedWing
Namespace: Aero
Syntax
[F,M] = forcesAndMoments(aircraft,state)
[F,M] = forcesAndMoments(aircraft,state,OutputReferenceFrame=outputReference)
Description
[
calculates the forces and moments of a fixed-wing aircraft, F
,M
] = forcesAndMoments(aircraft
,state
)aircraft
,
based around a state state
.
[
calculates the forces and moments using an output reference.F
,M
] = forcesAndMoments(aircraft
,state
,OutputReferenceFrame=outputReference
)
Input Arguments
Output Arguments
Examples
Version History
Introduced in R2021a